Space Hardware Marketplace — Satellite Platforms, Components & Ground Equipment — Page 107

Thermal Control

Gas Thermal Compressor

Allatherm

Gases handledKrypton, Xenon, Hydrogen, hydrocarbons
Output pressure200–400+ bar
Moving partsNone

Passive, vibration-free thermal compressors for Xenon, Krypton, and Hydrogen gases reaching 200–400+ bar — no moving parts for…

Thermal Control

Altom10 Series — LHP Evaporator Modules for Microelectronics

Allatherm

MaterialsCopper (Cu) and Stainless Steel (SS)
Charge chamber volume1–7 cc
Footprint range28×50 mm to 100×50 mm

Modular Loop Heat Pipe evaporator modules for microelectronics thermal management — up to 10 m separation, several thousand…

ADCS & Navigation

RWA05 Reaction Wheel Assembly

azista-bst-aerospace

TypeReaction wheel assembly with integrated fibre-optic gyro
ApplicationAttitude control of small satellites
Product lineAzista BST subsystems (BAT-110, PCU-110, PPDH-110, PLSU, RWA05)

Reaction wheel assembly for small satellites with integrated fibre-optic gyro, by Azista BST Aerospace.

OBC & Avionics

Payload Support Unit (PLSU)

azista-bst-aerospace

Input from payloadUp to 10 Gbit/s raw (LVDS, Camera Link, GigE, USB)
Storage1 TB, 850 MB/s write speed
Encryption128-bit AES-GCM, Diffie-Hellman-RSA 3072-bit

Electronic device operating payload data storage/processing/compression — up to 10Gbit/s input, 1TB storage, 128-bit AES-GCM encryption, CCSDS compliant.

Sun Sensors

ST200 Star Tracker

azista-bst-aerospace

InterfaceUART or RS422
Supply3.7-5V DC
Dimensions30x30x39 mm (with baffle: 50x50x83 mm)

One of the world's smallest fully autonomous star trackers — 10 arcsec pitch/yaw accuracy, 5Hz update rate, 100+…

EPS & Power Conditioning

PCU-110 Power Control Unit

azista-bst-aerospace

Main TMTC interfaceRS422
Solar panel power in (standard)20-25V DC
Regulated power (standard)24V, 12V, 5V, 3.3V

Flight-proven Power Control and Distribution Unit — adjustable switches/fuses, latch protection, optional MPPT, 5-year LEO design life.

Power Systems

BAT-110 Satellite Battery

azista-bst-aerospace

Size240 x 119 x 87 mm
Weight3000 g
Nominal voltage23.1 V (scalable to 12V, 15V, 18V, 28V)

Modular Li-FePO4 battery system for satellites — 10x more cycles than Li-Ion/Li-Po, radiation tested to 30 krad, 5-year…

SmallSat Platforms

LEOS-50 Satellite Platform

azista-bst-aerospace

Core volume570 x 570 x 200 mm
Mass50 kg
Design life5 years (LEO)

50kg-class LEO satellite bus — the workhorse of ABA satellites, 5°/s fast target pointing, X-band 1Gbps downlink, electrical…

SmallSat Platforms

LEOS-100 Satellite Platform

azista-bst-aerospace

Core volume600 x 600 x 200 mm
Mass150 kg
Design life5 years (LEO)

150kg-class satellite bus with body-mounted panels for high-precision instruments — 50cm GSD Earth observation, 2kW power, 5-year design…

Payloads & Instruments

ARS-16 Angular Rate Sensor / Dynapak-16

BlueHalo (Applied Technology Associates)

Minimum measurable angular motion40 nanoradians
Dynamic range>120 dB
Cross-axis angular sensitivityLow

Precision angular rate sensors for line-of-sight stabilization and jitter measurement — measures angular motion as low as 40…

Optical Communications

Laser Communications (Optical Comm Payloads)

BlueHalo (Applied Technology Associates)

Bandwidth advantage10-100x more than traditional RF communications

Space-qualified laser communication payloads — 10-100x more bandwidth than RF, low-jitter optical modules with proprietary inertial reference unit.

Optical Communications

Fast Steering Mirrors (FSM)

BlueHalo (Applied Technology Associates)

Aperture range15mm to 150mm
Orbit qualificationLEO
Companion controllerMANTIS (supports 2 FSMs simultaneously)

High-precision fast steering mirrors (15-150mm aperture) for low-jitter beam pointing in space-qualified optical communications and imaging.

Communications

BADGER Broad Area Deployable Ground Terminal

BlueHalo (Applied Technology Associates)

Orbital regimesGEO/MEO/LEO
Operational frequenciesL/S/C-Band
Scan angle±60 degrees

Deployable, software-defined multi-beam, multi-band phased-array ground terminal for resilient SATCOM — GEO/MEO/LEO support, ±60° scan angle.

Structures & Mechanisms

CubeSat Structure Development & Machining Service

Boltless CubeSat Structures (Kikuchiseiki, KIKUCHI SEIKI)

Delivery time3 weeks
ServicesTopology optimization analysis, machinability review, technical support

Custom CubeSat structural design-and-build service — topology optimization, precision machining, 3-week fast delivery of standard structure products.

Structures & Mechanisms

Boltless CubeSat Structure

Boltless CubeSat Structures (Kikuchiseiki, KIKUCHI SEIKI)

Rail precision50 µm
Supported form factors3U, 6U
Reliability collaborationUniversity of Tsukuba

Fastener-free CubeSat structural chassis for 3U and 6U platforms — no fastening parts, reliability assessed with University of…

Reaction Wheels

Propulsion and Attitude Control Systems

BHDynamics

ComponentsReaction wheels, magnetorquers, low-power thrusters

Attitude control and low-power propulsion solutions for PocketQubes and nanosatellites — reaction wheels, magnetorquers, and low-power thrusters.

Communications

SatComm Communications System

BHDynamics

Frequency bandsUHF, VHF
Additional protocolLoRa
FeaturesAdaptive modulation, error correction, high noise immunity

Space telecommunications system for PocketQubes and nanosatellites using RF (UHF/VHF) and LoRa technology — adaptive modulation, error correction.

OBC & Avionics

OBC for PocketQubes

BHDynamics

Key featuresLow power consumption, high efficiency, fast processing
ReliabilityRedundant memory, fault-tolerant design

High-performance On-Board Computer for PocketQubes and nanosatellites — optimized for low power and fast processing with redundant memory.